2015-12-30 18:57:56 -04:00
|
|
|
/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
|
|
|
|
|
2016-01-14 15:30:56 -04:00
|
|
|
#include "Sub.h"
|
2016-01-23 01:46:31 -04:00
|
|
|
#define LAND_END_DEPTH -20 //Landed at 20cm depth
|
2015-12-30 18:57:56 -04:00
|
|
|
|
|
|
|
// counter to verify landings
|
|
|
|
static uint32_t land_detector_count = 0;
|
|
|
|
|
|
|
|
// run land and crash detectors
|
|
|
|
// called at MAIN_LOOP_RATE
|
2016-01-14 15:30:56 -04:00
|
|
|
void Sub::update_land_and_crash_detectors()
|
2015-12-30 18:57:56 -04:00
|
|
|
{
|
|
|
|
// update 1hz filtered acceleration
|
|
|
|
Vector3f accel_ef = ahrs.get_accel_ef_blended();
|
|
|
|
accel_ef.z += GRAVITY_MSS;
|
|
|
|
land_accel_ef_filter.apply(accel_ef, MAIN_LOOP_SECONDS);
|
|
|
|
|
|
|
|
update_land_detector();
|
|
|
|
|
|
|
|
crash_check();
|
|
|
|
}
|
|
|
|
|
|
|
|
// update_land_detector - checks if we have landed and updates the ap.land_complete flag
|
|
|
|
// called at MAIN_LOOP_RATE
|
2016-01-14 15:30:56 -04:00
|
|
|
void Sub::update_land_detector()
|
2015-12-30 18:57:56 -04:00
|
|
|
{
|
2016-01-23 23:20:07 -04:00
|
|
|
if(barometer.num_instances() > 1 && barometer.get_altitude() > LAND_END_DEPTH && ap.throttle_zero) {
|
2016-01-23 01:46:31 -04:00
|
|
|
set_land_complete(true);
|
|
|
|
} else {
|
|
|
|
set_land_complete(false);
|
|
|
|
}
|
2015-12-30 18:57:56 -04:00
|
|
|
}
|
|
|
|
|
2016-01-14 15:30:56 -04:00
|
|
|
void Sub::set_land_complete(bool b)
|
2015-12-30 18:57:56 -04:00
|
|
|
{
|
|
|
|
// if no change, exit immediately
|
|
|
|
if( ap.land_complete == b )
|
|
|
|
return;
|
|
|
|
|
|
|
|
land_detector_count = 0;
|
|
|
|
|
|
|
|
if(b){
|
|
|
|
Log_Write_Event(DATA_LAND_COMPLETE);
|
|
|
|
} else {
|
|
|
|
Log_Write_Event(DATA_NOT_LANDED);
|
|
|
|
}
|
|
|
|
ap.land_complete = b;
|
|
|
|
}
|
2016-01-23 23:20:07 -04:00
|
|
|
|
|
|
|
// update_throttle_thr_mix - sets motors throttle_low_comp value depending upon vehicle state
|
|
|
|
// low values favour pilot/autopilot throttle over attitude control, high values favour attitude control over throttle
|
|
|
|
// has no effect when throttle is above hover throttle
|
|
|
|
void Sub::update_throttle_thr_mix()
|
|
|
|
{
|
2016-02-24 19:39:26 -04:00
|
|
|
return; // placeholder, was used by heli only
|
2016-01-23 23:20:07 -04:00
|
|
|
}
|